Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 9 - Stators
Patents for F01D 9 - Stators (10,038)
11/2007
11/29/2007WO2007135449A1 A turbine for a turbocharger
11/29/2007WO2007093851A3 Airfoil for a third stage nozzle guide vane
11/29/2007US20070274826 Diffusor
11/29/2007DE112004000100B4 Gekühlte Schaufeln eines Gasturbinentriebwerks -Cooled blades of a gas turbine engine
11/29/2007DE102006024783A1 Two-stage exhaust gas turbocharger for an internal combustion engine has an exhaust gas manifold and a high-pressure turbine in series in an exhaust gas' direction of flow
11/29/2007DE102006024782A1 Zweistufige Abgasturboladeranordnung Two-stage exhaust gas turbocharger assembly
11/29/2007DE102006024781A1 Zweistufige Abgasturboladeranordnung Two-stage exhaust gas turbocharger assembly
11/29/2007CA2589925A1 Guidance device for an inlet air flow to a combustion chamber in a turbine engine
11/28/2007EP1860325A1 Diffuser
11/27/2007US7300251 Turbine cooling vane of gas turbine engine
11/27/2007US7300247 Axial flow turbine
11/27/2007US7300246 Integrated turbine vane support
11/27/2007US7299617 Combustion chamber intermediate part for a gas turbine
11/21/2007EP1856376A1 Cooled transition duct for a gas turbine engine
11/21/2007CN101074609A Guiding device for waste gas turbocharger axial air intaking turbine
11/21/2007CN100350075C High-temperature protection layer
11/20/2007US7296397 Ventilation system for a convergent divergent exhaust nozzle
11/15/2007US20070264120 Device for tuning clearance in a gas turbine, while balancing air flows
11/14/2007EP1854960A1 Method and system for rotating a turbine stator ring
11/13/2007US7294361 Method and device for gas phase diffusion coating of metal components
11/13/2007US7293957 Vane platform rail configuration for reduced airfoil stress
11/08/2007WO2007127169A1 Stator vane having both chordwise and spanwise camber
11/08/2007DE102006020597A1 Housing for a waste gas turbine supercharger of an internal combustion engine comprises a gas inlet channel designed so that part of the incoming gas flows toward a separating wall onto a turbine blade
11/07/2007EP1852575A1 Stationary blade ring of axial compressor
11/07/2007EP1852572A2 Ceramic matrix composite turbine engine vane
11/07/2007CN101067384A Rotary machines and methods of assembling
11/07/2007CN101067383A Ceramic matrix composite vane seals
11/07/2007CN101067382A Methods and apparatus for thermal barrier coatings with improved overall thermal insulation characteristics
11/07/2007CN100347415C Casing of a turbocharger
11/07/2007CN100347414C Method of manufacturing steam turbine
11/07/2007CN100347411C Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade
11/06/2007US7291946 Damper for stator assembly
11/06/2007US7290983 Turbine, fixing device for blades and working method for dismantling the blades of a turbine
11/06/2007US7290982 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
11/06/2007US7290806 Assembly fixture
11/06/2007US7290337 Manufacturing method for frame body and frame body
11/06/2007CA2243333C Apparatus for ventilating a turbine stator ring
11/01/2007WO2007122022A1 Turbine blade
10/2007
10/31/2007EP1850070A2 Methods and system for reducing pressure losses in gas turbine engines
10/31/2007EP1849964A2 Gas turbine rotor containment element with frangible connections
10/31/2007EP1849963A2 Nested turbine bucket closure group
10/31/2007EP1849960A2 Turbine blade having internal cooling passage
10/31/2007CN101063414A Steam turbine and rotor
10/31/2007CN101063413A 蒸汽涡轮 Steam turbine
10/31/2007CN100346060C Guider of radial flow turbine
10/31/2007CN100346059C 涡轮叶片和燃气轮机 Turbine blades and turbine
10/30/2007US7287957 Inner shroud for the stator blades of the compressor of a gas turbine
10/30/2007CA2308400C C-shaped ring seal
10/25/2007US20070246183 Refractory metal core wall thickness control
10/24/2007EP1847697A1 Method and device for a gas turbine reheat system.
10/24/2007EP1847696A1 Component for a secondary combustion system in a gas turbine and corresponding gas turbine.
10/24/2007EP1847689A2 Apparatus and method of diaphragm assembly
10/24/2007EP1847687A1 Device for cooling a turbine casing of a turbomachine and a distributor therefore
10/24/2007EP1847685A2 Forward sleeve retainer plate and method
10/24/2007EP1847684A1 Turbine blade
10/24/2007EP1847681A2 Wedge repair of mechanically retained vanes
10/24/2007CN200964873Y Exhaust turbosupercharger transonic turbine for diesel locomotive
10/24/2007CN101059083A Apparatus and method of diaphragm assembly
10/24/2007CN101059082A Wedge repair of mechanically retained vanes
10/24/2007CN101059081A Turbine blade and diaphragm construction
10/23/2007US7284955 Fitting of distributor sectors in an axial compressor
10/18/2007DE102006016975A1 Mantel ring segment e.g. shroud, for use in e.g. aircraft engine, has two-sectional structure made of radial inner lying section and radial outer lying section, where sections exhibit different thermal expansion characteristics
10/17/2007EP1845236A2 Flap gasket for a turbo engine
10/17/2007CN101054908A Stator vane with variable setting of a turbomachine
10/17/2007CN100343490C Turbine nozzle retention apparatus at the carrier horizontal joint face
10/11/2007WO2007113149A1 Guide blade for turbomachinery, in particular for a steam turbine
10/11/2007WO2007113053A1 Guide blade segment of a thermal turbomachine, associated production method and thermal turbomachine
10/11/2007US20070237633 Vane assembly with grommet
10/11/2007US20070237632 Foreign object damage resistant vane assembly
10/11/2007US20070237631 Sacrificial inner shroud liners for gas turbine engines
10/10/2007EP1843010A2 Gas turbine compressor casing flowpath rings
10/10/2007EP1843009A1 Stator vane segment for a turbomachine, associated manufacturing method and turbomachine
10/10/2007EP1843008A1 Stator vane with variable setting of a turbomachine
10/10/2007CN101052784A Air inlet for turbine supercharger of internal-combustion engine
10/10/2007CN101050713A Closed loop, steam cooled turbine shroud
10/09/2007US7278827 Cooling air evacuation slots of turbine blades
10/09/2007US7278820 Ring seal system with reduced cooling requirements
10/09/2007US7278516 Apparatus and method for bearing lubrication in turbine engines
10/09/2007CA2333030C A rotor machine device
10/06/2007CA2583850A1 Turbine engine variable stator vane
10/04/2007US20070232327 Wireless terminal location using apparatus and methods employing carrier diversity
10/04/2007US20070231132 Device for attaching ring sectors to a turbine casing of a turbomachine
10/04/2007US20070231122 Turbine Nozzle Segment, Turbine Nozzle, Turbine, and Gas Turbine Engine
10/04/2007US20070227119 HPT aerodynamic trip to improve acoustic transmission loss and reduce noise level for auxiliary power unit
10/03/2007EP1840339A1 Device for attaching ring sectors around a turbine wheel of a turbomachine
10/03/2007EP1840337A1 Tongue and groove connection between two components of a turbine
10/03/2007EP1840329A1 Optimised synchronising ring vane, synchronising ring quadrant, compression stage, compressor and turbomachine comprising such a vane
10/03/2007EP1840328A1 Synchronising ring quadrant, compression stage, compressor and turbomachine comprising such a ring
10/03/2007CN101046162A Device for fixing ring sectors on the casing of a jet engine
10/03/2007CN101046161A Device for fastening ring sectors around a turbine wheel of a turbine engine
10/03/2007CN101045981A Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine
10/03/2007CN100340741C Turbine nozzle airfoil
09/2007
09/30/2007CA2583132A1 Apparatus for cooling the turbine casing of a turbine engine
09/30/2007CA2582621A1 Rectifier blade in custom-shaped location, rectifier sector, compression stage, compressor and turbine engine that comprises such a blade
09/30/2007CA2582401A1 Device for fastening ring sectors around a turbine wheel of a turbine engine
09/30/2007CA2582400A1 Optimized guide vane, guide sector, compression stage, compressor and turbine engine comprising said vane
09/30/2007CA2582398A1 Device for fastening ring sectors on a turbine housing of a turbine engine
09/29/2007CA2582638A1 Cooling jacket and blade assembly, turbine engine guide vanes comprising the assembly, turbine engine, assembly process and repair
09/27/2007WO2007108232A1 Turbine cascade end wall
09/27/2007US20070224045 Vehicle cooling fan
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